Future aspects of supersonic transport navigation
Supersonic transport navigation, guidance, and integrated avionics system
Pawlak, R. J.↗
SEARCH · Engineering Papers
Results for “NAVIGATION AND GUIDANCE”
Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.
Computer-controlled steering of the Apollo spacecraft.
Apollo spacecraft powered maneuvering controlled by digital computer as central element in guidance, navigation and control system
Battin, R. H.↗
Saturn launch vehicles astrionics system.
Saturn launch vehicles astrionics system, reviewing navigation, guidance, control and communication functions of electronic instrument on S-4B stage
Decher, R.↗
Computer-controlled steering of the Apollo spacecraft.
Apollo spacecraft powered maneuvering controlled by digital computer as central element in guidance, navigation and control system
Battin, R. H.↗
A performance study of the lunar module's landing radar system.
Lunar landing module Doppler radar system in guidance navigation and control system, studying mathematical model performance
Eichler, J.↗
A comprehensive digital simulation for the verification of Apollo flight software
Flight software for onboard Apollo Primary Guidance, Navigation and Control System flight qualification by digital simulation, including software diagnostics
Femino, S. R.↗
Apollo crew procedures, simulation, and flight planning
Apollo crew procedures, simulation and flight planning, discussing navigation, guidance and control procedures
North, W. J.↗
The Mariner Mars 1971 mission design
Mariner Mars 1971 mission design, discussing objectives, orbit selection, guidance, navigation and sequence analysis
Bollmann, W. E.↗
An engineering study of onboard checkout techniques. Task 5: Subsystem level failure modes and effects
Failure effects analysis of guidance, navigation, and control, data management, and communications subsystems
Frizzell, J. H.↗
A conceptual study of the SSV/GN&C system data bus
Development of time shared data bus concept for use with space shuttle guidance, navigation, and control system
Proch, G. E.↗
Influence of perturbing effects on a manual rendezvous system
Spacecraft navigation, guidance and control for manual rendezvous with orbiting target, examining error sources perturbing effects
Koble, H. M.↗
Computer requirements analysis and trade-offs for on-board space guidance and control systems
Computer requirements of self contained guidance, navigation and control system onboard manned orbital space station
Jurison, J.↗
Interactive Saturn flight program simulator
Interactive Saturn flight program simulator for real time graphics operations of navigation, guidance, engine control, event sequencing and communications
Dillon, T. J.↗
Operations and functions of the MINKEY rendezvous computer program in the Apollo command module computer
Minkey rendezvous computer program in Apollo 15 CSM aiding guidance, navigation and control system functions
Copps, S. L.↗
Modular space station detailed preliminary design. Volume 1: Sections 1 through 4.4
Detailed configuration and subsystems preliminary design data are presented for the modular space station concept. Each module comprising the initial space station is described in terms of its external and internal configuration, its functional responsibilities to the initial cluster, and its orbital build up sequence. Descriptions of the subsequent build up to the growth space station are also presented. Analytical and design techniques, tradeoff considerations, and depth of design detail are discussed for each subsystem. The subsystems include the following: structural/mechanical; crew habitability and protection; experiment support; electrical power; environmental control/life support; guidance, navigation, and control; propulsion; communications; data management; and onboard checkout subsystems. The interfaces between the station and other major elements of the program are summarized. The rational for a zero-gravity station, in lieu of one with artificial-gravity capability, is also summarized.
Source record↗
Space vehicle displays design criteria
The guidance, navigation, and control displays associated with manned spaceflight are summarized. Major emphasis were placed on methodologies useful for determining necessary information and its uses, systems analysis techniques, and analytic methods for design and evaluation of such systems.
Source record↗
Telemetry and the integrated avionics approach.
The unique problems encountered in the integrated approach to aircraft and spacecraft avionics system designs are discussed with the emphasis on recent advances in telemetry as a factor facilitating the integration. A listing of subsystems planned for integration on the Space Shuttle vehicle is given, covering auxiliary pumping and propellant, crew controls and displays, computation, communications and radar, electric power, guidance, navigation and control, air-bearing engines, main engines, reaction control, and structural/mechanical elements. Considerations are given for the multiplexed data bus design applicable to integrated avionics.
Frost, W. O.↗
Research and Applications Module (RAM) phase B study. Preliminary design review brochure
A briefing is presented of the preliminary design of the selected Research and Applications Module (RAM) concepts, operations, and missions of the sortie and free-flying RAM. Included are the study program plan, program objectives, guidelines, source of payloads, mission requirements, shuttle performance, guidance navigation and control, propulsion, and costs.
Source record↗